The Defence Aviation Safety Program Manual

Volume 2: Defence Aviation Safety Regulation

Introduction

Purpose

This Volume establishes requirements for the management of Defence Aviation Safety by commanders and managers. 

Structure

The Defence Aviation Safety Regulation (DASR) is comprised of: 

General Requirements (GR), which are set out below in two subparts:

Subpart A Scope and applicability defines the scope of the DASR and the applicability of the DASR parts.

Subpart B Common requirements and provisions establishes requirements and provisions that are each applicable to a significant proportion of regulated entities.

the DASR parts, which are set out in Annex A.

DASR clauses and sub-clauses may have associated supporting information in the form of:

Acceptable Means of Compliance (AMC). AMC is information published by DASA to identify a means of meeting one or more requirements of the DASR. Regulated entities are not required to comply with AMC and may instead propose an Alternative Means of Compliance to DASA. Any such proposal will be subject to separate assessment by DASA to determine whether the approach is compliant with the DASR.

Guidance Material (GM). GM provides additional explanation to assist the application of the requirement and/or explain the AMC.

Context

This Volume implements applicable requirements set out in DASP Manual Volume 1 Requirements for the DASP.

DASP Manual Volume 3 DASP Guidance provides further information to support understanding of, and compliance with, the DASR.

Definitions

The following definitions apply within this Volume and its annex:

Continuing Airworthiness. All of the processes ensuring that, at any time in its operating life, an aircraft complies with the airworthiness requirements in force and is in a condition for safe operation.

Defence Personnel. All Australian Public Service employees in the Department of Defence, Defence locally engaged employees, Defence civilians, Defence members and the equivalents from other Defence organisations on exchange to Defence. 

Defence Registered Aircraft. An aircraft listed on the Defence aircraft register maintained by DASA.

State Aircraft. Aircraft of any part of the Defence Force (including any aircraft that is commanded by a member of that Force in the course of duties as such a member); and aircraft used in the military, customs or police services of a foreign country.  This includes Uncrewed Aircraft Systems (UAS). 

Further definitions are available in the DASP Glossary.

General Requirements

Subpart A: Scope and applicability

GR.10 Aircraft registration

State Aircraft operated by Defence must be:

Defence Registered Aircraft; or

managed in accordance with DASR NDR Non-Defence Registered aircraft.

Paragraph (a) is not applicable to Uncrewed Aircraft Systems except as required by DASR UAS Uncrewed Aircraft Systems.

GR.15 Airworthiness of Defence Registered Aircraft

The design, production and certification of Defence Registered Aircraft must be managed in accordance with DASR 21 Aircraft Design, Production and Certification.

The Continuing Airworthiness of Defence Registered Aircraft, and components thereof, must be managed in accordance with:

DASR M Continuing Airworthiness Management

DASR 145 Requirements for Maintenance Organisations

DASR 66 Military Aircraft Maintenance Licencing

DASR 147 Aircraft Maintenance Training Organisations.

By way of exception from DASR GR.15 (a) and (b), the operator of a Defence Registered aircraft in one of the following categories may demonstrate airworthiness management that achieves a level of Aviation Safety at least equivalent to comparable Australian civil registered aircraft: AMCAMC

AMC GR.15(c) Airworthiness of Defence Registered Aircraft

Compliance documentation

The MAO should demonstrate compliance with DASR GR.15(c) through an annex to the respective MAO Operations Compliance Statement (OCS).

Airworthiness Management of Crewed Hot Air Balloons

Introduction

This AMC identifies an approach to the airworthiness management of Defence Registered crewed hot air balloons through tailoring of applicable DASR parts. This approach meets or exceeds the level of Aviation Safety established by CASR 131 for balloon transport operations. 

This AMC is intended for application to aircraft for which DASA will issue, or has issued, a Certificate of Airworthiness against a type-certificate issued by a recognised Civil Aviation Authority (CAA); ie where DASA has not issued a Military Type Certificate. Accordingly, all references to a CAA, type-certificate or type-certificate holder should be interpreted in the context of the relevant civil type-certificate.

Responsible personnel

The MAO Accountable Manager (MAO-AM) must nominate an Approved Person responsible for ensuring the airworthiness management of Defence Registered crewed hot air balloons operated by the MAO.

The Approved Person must be formally accepted by DASA through a DASR Form 4 Acceptance of Nominated Management Personnel. The Approved Person should have: 

practical experience and expertise in the application of Australian civil aviation regulations as applicable to a civil balloon transport operator

practical experience and expertise in the application of applicable DASR

an appropriate understanding of the Airworthiness Review process and the requirements to conduct an Airworthiness Review

knowledge of:

the airworthiness and maintenance requirements for the relevant aircraft operated by the MAO

the need for, and content of, the relevant parts of the MAOC OCS when applicable. 

Recognition of other aviation authorities

The MAO may leverage the DASA recognition framework to accept Initial and Continuing Airworthiness products and services provided by, or under the approval of, a recognised aviation authority. Details of recognised authorities are available on the DASA recognition web site.
Initial Airworthiness

A MAO intending to operate a Defence Registered crewed hot air balloon for which a civil type-certificate is in force should apply to DASA for the issue of a Military Certificate of Airworthiness on the basis of that civil type-certificate under DASR 21.A.174(c)4.

Continuing Airworthiness

The operator of a Defence Registered crewed hot air balloon may ensure Continuing Airworthiness through tailored application of DASR M Continuing Airworthiness Management as follows:

M.A.201 Responsibilities is applicable in its entirety except for paragraph M.A.201(h). Maintenance organisations ‘accepted by DASA’ under M.A.201(g) should be understood to include organisations that hold a Certificate of Approval issued under Regulation 30 of the Civil Aviation Regulations 1988.

M.A.301 Continuing airworthiness tasks is applicable in its entirety, tailored as follows:

paragraph M.A.301(a)4 is not applicable

for paragraph M.A.301(b)1, ‘the requirements of DASR M’ should be understood to mean the tailored requirements set out in this AMC.

DASR M.A.302 Aircraft Maintenance Programme (AMP) is not applicable; however, the MAO must use suitable maintenance publications and data approved by the relevant type-certificate holder or CAA.

M.A.303 Airworthiness Directives is applicable in its entirety. An ‘applicable Airworthiness Directive’ should be understood to include Airworthiness Directives and equivalent documents issued by the aviation authority that issued the relevant civil type-certificate.

M.A.304 Data for modifications and repairs is applicable in its entirety. ‘An organisation accepted by the MAA’, as referenced in paragraph M.A.304(d), should be understood to include any person or organisation appropriately approved by a recognised aviation authority.

M.A.305 Aircraft Continuing Airworthiness record system is applicable in its entirety. A ‘Certificate of Release to Service’ is replaced by ‘authorised release certificate’. An ‘aircraft continuing airworthiness record system’ is replaced by ‘balloon log book’.

M.A.306 Aircraft technical log is applicable in its entirety except for references to DASR M.A.305 Aircraft Continuing Airworthiness record system.

M.A.307 Transfer of aircraft Continuing Airworthiness records is applicable in its entirety. 

Subpart I Military Airworthiness Review Certificate (MARC), comprising M.A.901 to M.A.905, is applicable in its entirety. References to the CAMO should be understood to mean the hot air balloon operator.

Tailored Airworthiness Review

Purpose. This section provides tailored Airworthiness Review requirements that should be read in conjunction with, and which take precedence over, Subpart I of DASR M.

Authorised personnel. The Approved Person must conduct the Airworthiness Review required for recommending the issue of a MARC. On completion of the Review, the Approved Person should complete DASR Form 15c Military Airworthiness Review Certificate Record and submit it to DASA.

Review of Aircraft records. A review of the aircraft records must be carried out to ensure that: 

aircraft flying hours, associated flight cycles, and any other airworthiness data have been properly recorded

the Aircraft Flight Manual is applicable to the aircraft configuration and reflects the latest revision status 

all the maintenance due on the aircraft according to the maintenance requirements have been carried out

any ongoing permissible unserviceabilities are managed 

all applicable Airworthiness Directives and equivalent requirements have been registered and appropriately incorporated 

all service-life-limited components installed on the aircraft are identified, tracked and have not exceeded the approved limit 

all maintenance has been released in accordance with applicable requirements

the aircraft weight and balance reflects the current configuration of the aircraft and is valid

the aircraft complies with the latest revision of the type-certificate associated with the Military Certificate of Airworthiness.

Physical Survey. A physical survey of the aircraft must be carried out to ensure that: 

all required markings and placards are properly installed

the Aircraft configuration is in compliance with the Aircraft Flight Manual

the Aircraft configuration is in compliance with the approved data

no evident defect identified that is not reasonably expected

no inconsistencies can be found between the Aircraft and Aircraft records.

crewed hot air balloons used in balloon transport operations under Part 131 of the Civil Aviation Safety Regulations 1998 (CASR)

Warbird, Historic and Replica Aircraft operated under CASR Part 132.

GR.20 Operations personnel

Personnel and organisations involved in Defence aviation operations must comply with:

DASR Aircrew

DASR MED Medical

DASR AVFM Aviation Fatigue Management

DASR NTS Non-Technical Skills.

Paragraph (a) is not applicable to Uncrewed Aircraft Systems except as required by DASR UAS Uncrewed Aircraft Systems.
 

GR.25 Operation of State Aircraft

The operation of State Aircraft by Defence must be in accordance with:

DASR AO.Gen Air Operations – General

DASR ARO Authority Requirements for Air Operations

DASR ORO Organisation Requirements for Air Operations

DASR NDR Non-Defence Registered aircraft

DASR SPA Specific Purpose Approval

DASR SPO Special Purpose Operations

DASR UAS Uncrewed Aircraft Systems

DASR FT Flight Tests

DASR ACD Air Cargo Delivery

DASR RoA Rules of the Air.

Defence Registered Aircraft must have a valid type-certificate11Including applicable restricted type-certificates issued in accordance with DASR 21 Subpart B.  to conduct operations. The type-certificate must be issued in accordance with DASR 21 Subpart B Military Type-Certificates and Military Restricted Type-Certificates.  

Defence Registered Aircraft must have a valid certificate of airworthiness22Including applicable restricted certificates of airworthiness issued in accordance with DASR 21 Subpart H  to conduct operations. The certificate must be issued in accordance with DASR 21 Subpart H Military Certificates of Airworthiness and Military Restricted Certificates of Airworthiness.

By way of exception from paragraph (c), an aircraft may be operated where a valid permit to fly has been issued. Any such permit to fly must be issued in accordance with DASR 21 Subpart P Military Permit to Fly. 

By way of exception from paragraph (c), UAS may be operated without a type-certificate or certificate of airworthiness, provided they are compliant with DASR UAS.10.

GR.27 Operation of Foreign Military Aircraft (FMA) in Australia 

GMGM

GM GR.27 – Foreign military operations in Australia

Purpose: (Context) Foreign Military Aircraft (FMA) are often approved to operate in Australian territorial airspace. However, foreign personnel can have limited familiarity with Australian airspace requirements and safety obligations to other airspace users and people on the ground. (Hazard) Ineffective Sponsor risk management of FMA in Australian airspace can compromise the safety of other airspace users and people on the ground. (Defence) This regulation places requirements on Sponsors of FMA in Australian airspace, to support compliance with the Work Health and Safety (WHS) Act 2011 (Cth), as it relates to the safety of other airspace users and people on the ground.\

All FMA involvement must have an associated Sponsor (ie an Officer IAW s27 of the Work Health and Safety (WHS) Act 2011 (Cth)), who is accountable for assessing and managing risk to the safety of other airspace users and people on the ground. Therefore, the Sponsor must be reasonably informed—ie have knowledge about the hazard and risks, and ways of eliminating or minimising the risks posed by FMA to the safety of other airspace users and people on the ground. The choice of Sponsor is a matter for command.

Applicability. This regulation applies to the Sponsor of FMA in Australian territorial airspace, including landing on Defence vessels (whether inside or outside Australian territorial waters).

 This regulation does not apply to FMA:

that are transiting through Australian territorial airspace (including stopovers)

that are used for diplomatic purposes only, or as a static display as part of their time in Australian territorial airspace (eg Aircraft used by a visiting state dignitary that will remain parked until the state visit is completed, or a FMA used only as a static display Aircraft at an air show).

The Sponsor who approves FMA to operate in Australian territorial airspace must:

ensure that FMA operations are conducted in a manner such that risks to the safety of other airspace users and people on the ground are eliminated So Far As is Reasonably Practicable (SFARP) and, where not reasonably practicable to eliminate, minimised SFARP GMGM AMCAMC

AMC GR.27(a)1 – Sponsor risk management

Sponsor risk management of FMA in Australian territorial airspace should include:

being informed by:

DASA’s recognition of the foreign MAA

open source data, if the foreign MAA is not recognised by DASA (DASA can provide support on request)

previous direct observations of the foreign military (eg through operations, exercises, exchanges or loans, or Defence representatives overseas)

conducting:

risk management:

for the scope of the FMA’s involvement, roles, tasks and environment 

IAW the ‘safety risk management process’ defined in DASA AC 003/2018 

continuous risk monitoring and review—IAW ‘step 7’ of the safety risk management process:

tailored relative to the level of risk exposure

on a recurring schedule (eg an annual (or similar) basis), when FMA remain in Australian territorial airspace continuously for six or more months, or remain temporarily but on a recurring basis—for example for RSAF 130SQN, SADFO RAAF Pearce invites 130SQN representatives to Base Aviation Safety Committee meetings  

engagement with relevant command or HQ’s ‘Director Legal’ (or equivalent appointment) during exercise concept design conferences, operational planning teams, or similar; to seek written authority for the foreign nation to abide by safety direction IAW DASR GR.27 (eg through Status Of Forces Agreements, Technical Arrangements, Memoranda of Understanding, Exercise or Operation Orders, etc)

considering additional safety controls as necessary

informing the sponsored organisation of:

safety controls (including limitations) imposed through the Sponsor’s Authority to Operate (AUTHOP)

Aviation Safety Event reporting and incident control requirements (inclusive of hazardous material information required by first responders), in consultation with DFSB

Australian Rules of the Air

airspace and environmental conditions and limitations

the Sponsor’s obligation to suspend FMA operations when there is concern that safety may be compromised

the Sponsor’s point-of-contact.

GM GR.27(a)1 – Sponsor risk management 

Sponsor RFIs. The Sponsor’s risk management of the FMA should occur well in advance of the FMA’s anticipated in-country arrival. This is to enable the Sponsor to submit any RFIs early to the foreign operating unit, as necessary (to inform the Sponsor’s risk assessment). Sponsors should not wait for the foreign operating unit to submit a request for a Diplomatic Clearance (DIPCLR) before submitting RFIs—as foreign operating units may submit DIPLCLR requests at short notice.

Organisations and appointments issuing invitations for FMA. Organisations and appointments issuing invitations for FMA should identify and consult with Sponsors prior to extending invitations—to enable safety risk management without undue risks to either:

other airspace users and people on the ground

the adverse international engagement effects of retrospectively withdrawing or curtailing the scope of an invitation.

On request, DASA can provide:

a list of recognised countries

a list of familiar aircraft types

information on previous Sponsor’s relevant FMA risk assessments (DASA maintains a central repository—drawn from DASR Form 140 submissions).

These lists and information:

inform appointments and organisations issuing invitations as to which countries AUS could invite without a significant risk of intrusive Sponsor controls (including to the point of effectively excluding participation in the relevant activity)

provide an indication of when appointments and organisations should consult with DASA before making an invitation/commitment to an international partner.  

Proactive Sponsor risk management of FMA.

During planning activities.

DASA MAA recognition. DASA’s MAA recognition promotes awareness, efficiency and flexibility, while maintaining an established level of credible and defensible safety assurance. The goal of recognition is to understand similarities and differences in the assessed MAA and its system, providing confidence that the foreign operator is working within a suitable safety framework with independent oversight. The basis of recognition is a top-down systems assessment, using an internationally agreed (open source) set of questions (Military Airworthiness Recognition Questions—MARQ), culminating in a published recognition certificate and relevant provisions (ie recognition scope, conditions and caveats). In turn, the regulated community can exploit this information to ensure the suitability of their specific Aviation Safety requirements.

In addition to leveraging from DASA’s recognition of the MAA, Sponsors should conduct their own assessment of the FMA and its operation— informed by experience from previous and current operations and exercises, open sources, and RFIs.

Operation/exercise concept design. Major Defence exercises and operations are planned through concept design conferences, operational planning teams, or similar. Such planning includes reviewing extant international agreements/arrangements (eg enduring Status Of Forces Agreements, Technical Arrangements and Memoranda Of Understanding) and the need for supplemental agreements/arrangements specific to an operation or exercise. The Sponsor should seek for any updated documents to include written authority for the foreign nation to abide by any safety directions imposed IAW DASR GR.27. 

Where concept design conferences are not held, or where formal agreements are not required/will not include written authority for the foreign nation to abide by safety directions imposed IAW DASR GR.27, Sponsors may alternatively choose to either:

include this requirement in the Exercise or Operation Orders (or equivalent)

write a letter to the relevant foreign operating unit (the unit which has command of the FMA), seeking agreement to comply with Sponsor direction (as a condition of access to Australian territorial airspace).

Direct observations of the foreign military. Previous direct observations of the foreign military (through exercises or operations (and relevant post activity reports), exchanges, loans, etc) can inform the Sponsor’s consideration of additional safety controls and operational limitations.

RFIs. RFIs on aviation safety topics, raised in planning correspondence to the foreign operating unit, can inform the Sponsor’s consideration of safety controls and operational limitations. Some example past RFIs include the foreign military’s:

Aircraft Type crew duty limits

deployed AVMO arrangements, and likely need to access local AVMO services

minimum on-board emergency fuel policy in Australian territory

Dangerous Goods carriage policy.

UAS. The level of safety implicit in DASR UAS provides a suitable benchmark for the Sponsor to execute their responsibilities. That is, a Sponsor could identify which UAS category an equivalent Defence UAS would operate within, and use this equivalent categorisation as a basis for assessing the foreign UAS operator’s risk controls. For example, where a foreign UAS operation is within the scope of a ‘specific category’ Standard Scenario, or within scope of the ‘open’ category, the Sponsor should confirm the FMA has implemented each of the standard operating conditions for that category.

Pre and during FMA Flights in Australian territorial airspace.

Use of ADF air riders and other liaison staff for FMA. Use of ADF air riders and other liaison staff (interpreter or otherwise) can provide an effective safety control of FMA (against the hazards FMA pose to the safety of other airspace users and people on the ground), for a pre-agreed scope and duration/exposure—pending the relevant foreign command’s acceptance. Note that the carriage of air riders and other liaison staff may be subject to CDF Directive 12/16.

Visual confidence inspections. Where necessary, targeted and informal visual confidence inspections of the FMA can validate the ability of the FMA to safely operate in Australian territorial airspace.

Operational limitations. Operational limitations can provide effective safety controls (eg foreign fast jet Aircraft may be based at RAAF Base Tindal and be required to transit to and from the designated training area via routes constrained to sparsely populated areas where possible).

Where the foreign MAA is not recognised by DASA. Where the foreign MAA is not recognised by DASA, CDF Directive 12/16 provides additional reference sources that Sponsors may use to inform the required safety controls. DASA can provide support on request.   
 

issue an Authority to Operate (AUTHOP) to document controls that manage the safety of other airspace users and people on the ground GMGM AMCAMC

AMC GR.27(a)2 – Sponsor’s Authority to Operate (AUTHOP)

Sponsors of FMA should:

use DASR Form 140 to issue an Authority To Operate (AUTHOP), and to:

advise DASA, before FMA Flights in Australian territorial airspace commence, of the intent to Sponsor FMA (note, DASA’s registration of the AUTHOP is not a prerequisite to issuing the Sponsor’s approval)

document the outcomes of the Sponsor’s safety risk management 

coordinate transfers of sponsorship as necessary.

GM GR.27(a)2 – Sponsor’s Authority to Operate (AUTHOP)

The purpose of an AUTHOP is to document the Sponsor's consideration of risks to the safety of other airspace users and people on the ground. The AUTHOP should define:

the FMA being approved and the means of compliance with DASR GR.27—including the safety controls the Sponsor has implemented

any FMA Sponsorship transfers, where necessary (eg joint and combined land and ship-based operations may require different Sponsors). 

Sponsor AUTHOP information assists DASA to maintain a register of FMA in Australian territorial airspace, and documents Sponsor details in case of an Aviation Safety Event.

monitor the effectiveness of controls against the risk to the safety of other airspace users and people on the ground; and any significant safety events—and suspend FMA operations when there is concern that safety may be compromised. AMCAMC

AMC GR.27(a)3 – Suspension of FMA Flight operations (AUS)

Suspension of Flight operations. The Sponsor suspending Flight operations should advise relevant Service commands and DASA as soon as practicable, including the proposed criteria and plan for resuming operations. Sponsors should consider the principles of AMC ARO.55.A - Cessation of Flight Operations (AUS) when suspending FMA Flight operations.

Resumption of Flight operations. Sponsors should consider the principles of AMC ARO.55.A - Cessation of Flight Operations (AUS) when resuming FMA Flight operations.

GR.30 Flight Simulation Training Devices

Flight Simulation Training Devices and their use must be managed in accordance with DASR FSTD Flight Simulation Training Devices.

GR.35 Aerodromes

Defence Aerodromes, including shipborne heliports, must be operated, managed and certified in accordance with DASR 139 Aerodromes.

GR.37 Air Navigation Services

The provision of Air Traffic Management services and Air Navigation Services by Defence, including equipment, systems, and organisations must be in accordance with:

DASR ANSP Air Navigation Service Providers; and

the regulations identified by GR.20 Operations personnel, as applicable.

GR.38 Air Battle Management

The provision of Air Battle Management operations conducted by Defence, including equipment, systems and organisations, must be in accordance with:

DASR ABM Air Battle Management

the regulations identified in GR.20 Operations personnel, as applicable

DASR AO.GEN.05 Management of OIP.

Subpart B: Common requirements and provisions

GR.40 Occurrence reporting

Where required by other DASR, regulated entities must report aviation safety occurrences to DASA in a form and manner acceptable to DASA.AMCAMC

AMC GR.40 – Occurrence Reporting

Intent

AMC GR.40 identifies which aviation safety occurrences should be reported to the Authority, and details the timescale for submission of such reports. It also describes the objective of the overall occurrence reporting system including internal and external functions.

Applicability

This AMC applies to occurrence reporting by persons / organisations regulated by the Defence Aviation Safety Regulation (DASR). In most cases the obligation to report is on the holders of a certificate or approval, which are primarily organisations, but in some cases may be an individual. In addition some reporting requirements are directed to persons. However, in order not to complicate the text, only the term ‘organisation’ is used throughout this AMC.

NOTE: This AMC does not apply to dangerous goods or explosive ordnance reporting.

Objective of Occurrence Reporting

The occurrence reporting system is an essential part of the overall monitoring function. The objective of the occurrence reporting, collection, investigation and analysis systems described in operating and airworthiness regulation, is to use the reported information to contribute to accident prevention, the improvement of aviation safety, and not to attribute blame, or take other enforcement actions.

The detailed objectives of the occurrence reporting systems are:

To enable an assessment of the safety implications of each occurrence to be made, including previous similar occurrences, so that any necessary action can be initiated. This includes determining what and why it had occurred and what might prevent a similar occurrence in the future.

To ensure that knowledge of occurrences is disseminated so that others may learn from them.

The occurrence reporting system is complementary to the normal day to day procedures and 'control' systems and is not intended to duplicate or supersede any of them. The occurrence reporting process is to identify those occasions where controls have failed.

Occurrences should remain in the databases when judged non-reportable by the person submitting the report as the significance of such reports may only become obvious at a later date.

Reporting to the Authority

Requirements:

Occurrences are defined as an incident, malfunction, defect, technical defect or exceedance of limitations that endangers or could endanger the safe operation of aircraft and must be reported to the Authority.

Reporting does not remove the reporter’s or organisation’s responsibility to commence corrective actions to prevent similar occurrences in the future. Known and planned preventive actions should be included within the report.

NOTE: Section I to IV of this AMC identifies what should be reported by an organisation or individual to the Authority.

Notifying Other Authorities

Where applicable and relevant, other (domestic and international) civil and military aviation safety authorities should be advised of the occurrences.

Reportable Occurrences

General. There are different reporting requirements for operators (and/or commanders), maintenance organisations, design organisations and production organisations. The criteria for all these different reporting lines are not the same. For example, the Authority will not receive the same kind of reports from a design organisation as from an operator or an Air Navigation Service Provider. This is a reflection of the different perspectives of the organisations based on their activities.

Many of the occurrences which are considered ‘reportable occurrences’ for crewed aircraft would not endanger safe operation of a UAS due to the absence of people on board. As such, reportable occurrences for UAS are found in the UAS implementing regulations.

List of reportable occurrences. Section I to IV is a list of reportable occurrences. Not all examples are applicable to each reporting organisation.

 Section I - Aircraft Flight OperationsSection I - Aircraft Flight Operations

Section I to AMC GR.40 - Aircraft Flight Operations

Under DASR Phase 1, reporting of Aircraft Flight Operations based occurrences using the Hazard Reporting and Tracking framework articulated within the Defence Aviation Safety Manual, and supporting procedures meets the intent of this SECTION.

A listing of specific Authority reportable Aircraft Flight Operations based occurrences will be consulted / promulgated in 2018.

 Section II - Aircraft TechnicalSection II - Aircraft Technical

Section II to AMC GR.40 - Aircraft Technical

This section is structured in such a way that the pertinent occurrences are linked with categories of activities during which they are normally observed, according to experience, in order to facilitate the reporting of those occurrences. However, this presentation must not be understood as meaning that occurrences must not be reported in case they take place outside the category of activities to which they are linked in the list.

Structural

For Structural Integrity (SI), an unsafe condition is not always obvious. Engineering judgement is required to decide whether defects or damage is serious enough to be reported, if in doubt advice should be sort. The following examples can be taken into consideration:

Defect or damage that may affect structural strength or life, to critical structure exceeding admissible damage or where no pre-approved repair exists from previous investigation activity. Critical structure is that which contributes significantly to carrying flight, ground, and pressurisation loads, and whose failure could result in a catastrophic failure of the aircraft.

Damage to or defect exceeding allowed tolerances of structural element which failure could reduce the structural stiffness to such an extent that the required flutter, divergence or control reversal margins are no longer achieved.

Damage to or defect of a structural element, which could result in the liberation of items of mass that may injure occupants of the aircraft.

Damage to or defect of a structural element, which could jeopardise proper operation of systems. See SYSTEMS (including software) below.

Loss of any part of the aircraft structure in flight.

Systems (including software)

The following generic criteria applicable to all systems are proposed: Loss, significant malfunction or defect of any system, subsystem or set of equipment that could endanger flight safety when standard operating procedures, drills etc, could not be satisfactorily accomplished.

Inability of the crew to control the system, for example:

uncommanded actions;

incorrect and or incomplete response, including limitation of movement or stiffness;

runaway;

mechanical disconnection or failure.

Failure or malfunction of the exclusive function(s) of the system (one system could integrate several functions).

Interference within or between systems.

Failure or malfunction of the protection device or emergency system associated with the system.

Loss of redundancy of the system.

Any occurrence resulting from unforeseen behaviour of a system.

Leakage of hydraulic fluids, fuel, oil or other fluids which resulted in a fire hazard or possible hazardous contamination of aircraft structure, systems or equipment, or risk to occupants.

Malfunction or defect of any indication system when this results in the possibility of misleading indications to the crew.

Any failure, malfunction or defect if it occurs at a critical phase of flight and relevant to the operation of that system.

Asymmetry of flight controls; eg flaps, slats, spoilers.

Enclosure 1 to SECTION II, gives a list of examples of reportable occurrences resulting from the application of these generic criteria to specific systems.

Propulsion Systems (including engines, propellers, rotor systems and transmissions) and Auxiliary Power Units (APU)

Engines. The following criteria applicable to engines are proposed:

Overspeed or inability to control the speed of any high speed rotating component, for example: auxiliary power unit, air starter, air cycle machine, air turbine motor, propeller or rotor.

Failure or malfunction of any part of an engine or powerplant resulting in any one or more of the following:

non containment of components/debris;

uncontrolled internal or external fire, or hot gas breakout;

thrust in a different direction from that demanded by the pilot;

thrust reversing system failing to operate or operating inadvertently;

inability to control power, thrust or rpm;

failure of the engine mount structure;

partial or complete loss of a major part of the powerplant;

Dense visible fumes or concentrations of toxic products sufficient to incapacitate crew or passengers;

inability, by use of normal procedures, to shutdown an engine;

inability to restart a serviceable engine.

A flameout, uncommanded thrust/power loss or malfunction:

for a single engine aircraft; or

where it is considered excessive for the application, or

where this could affect more than one engine in a multi-engine aircraft, particularly in the case of a twin engine aircraft; or

for a multi engine aircraft where the same, or similar, engine type is used in an application where the event would be considered hazardous or critical.

Any defect in a propulsion system critical part causing retirement before completion of its full life.

Defects of common origin which could cause an in flight shut down rate so high that there is the possibility of more than one engine being shut down on the same flight.

An engine limiter or control device failing to operate when required or operating inadvertently.

Exceedance of engine parameters.

Volcanic ash encounter.

Propellers and transmission.

Failure or malfunction of any part of a propeller or powerplant resulting in any one or more of the following:

an overspeed of the propeller;

the development of excessive drag;

a thrust in the opposite direction to that commanded by the pilot;

a release of the propeller or any major portion of the propeller;

a failure that results in excessive unbalance;

the unintended movement of the propeller blades below the established minimum in-flight low-pitch position;

an inability to feather the propeller;

an inability to command a change in propeller pitch;

an uncommanded change in pitch;

an uncontrollable torque or speed fluctuation;

The release of low energy parts.

Rotors and transmission:

Damage or defect of main rotor gearbox or attachment which could lead to in flight separation of the rotor assembly, and /or malfunction/loss of rotor control.

Damage or defect to tail rotor, transmission and equivalent systems.

Auxiliary Power Units:

Shut down or failure when the APU is required to be available by operational requirements, eg Defence Long Range Operations (DLRO) / Extended Twin-engined Operations (ETOPS) / Extended Range Operations (EROPS), Minimum Equipment List (MEL).

Inability to shut down the APU.

Overspeed.

Inability to start the APU when needed for operational reasons.

 

ENCLOSURE 1 TO SECTION II - REPORTABLE TECHNICAL OCCURRENCES TO SPECIFIC SYSTEMS

The following give examples of reportable occurrences resulting from application of the generic criteria to specific systems listed under SYSTEMS (including software), in SECTION II.

Air conditioning / ventilation

complete loss of avionics cooling

depressurisation

Autoflight system

failure of the autoflight system to achieve the intended operation while engaged

significant reported crew difficulty to control the aircraft linked to autoflight system functioning

failure of any autoflight system disconnect device

uncommanded autoflight mode change

Bleed air system

hot bleed air leak resulting in a fire warning or structural damage

loss of bleed air systems

failure of bleed air leak detection system

Cockpit / cabin / cargo

pilot seat control loss during flight

failure of any emergency system or equipment, including emergency evacuation

signalling system, all exit doors, emergency lighting, etc

loss of retention capability of cargo loading system

Communications

total loss of communication in flight

Electrical system

loss of one electrical system distribution system (AC or DC)

total loss or loss of more than one electrical generation system

failure of back-up (emergency) electrical generating system

serious damage to electrical wiring and interconnection system (EWIS)

Explosive ordnance

inadvertent release of stores due to mechanical or system failure

hung store

stores management system failure

Fire protection system

fire warnings, except those immediately confirmed as false

undetected failure or defect of fire/smoke detection/protection system, which could lead to loss or reduced fire detection/protection

absence of warning in case of actual fire or smoke

Flight controls

asymmetry of flaps, slats spoilers, etc

limitation of movement, stiffness or poor or delayed response in the operation primary

Flight control surface runaway

mechanical flight control disconnection or failure

significant interference with normal control of the aircraft or degradation of flying qualities

Fuel system

fuel quantity indicating system malfunction resulting in total loss or erroneous indicated fuel quantity on board

leakage of fuel which resulted in major loss, fire hazard, significant contamination

malfunction or defects of the fuel jettisoning system which resulted in advertent loss of significant quantity, fire hazard, hazardous contamination of aircraft equipment or inability to jettison fuel

fuel system malfunctions or defects which had a significant effect on fuel supply and/or distribution

Hydraulics

loss of one hydraulic system (extended twin-engined operations (ETOPS) only)

failure of the isolation system to operate

loss of more than one hydraulic circuit

failure of the back-up hydraulic system

inadvertent Ram Air Turbine extension

Ice detection / protection system

undetected loss or reduced performance of anti ice/de-ice system

loss of more than one of the probe heating systems

inability to obtain symmetrical wing de-icing

abnormal ice accumulation leading to significant effects on performance or handling qualities

crew vision significantly affected

Indicating / warning / recording systems

malfunction or defect of any indicating system when the possibility of significant misleading indications to the crew could result in an inappropriate crew action on an essential system

for glass cockpits: loss or malfunction of more than one display unit or computer involved in the display/warning function

Landing gear system / brakes / tyres

brake fire

significant loss of braking action

unsymmetrical braking leading to significant path deviation

failure of the landing gear free fall extension system (including during scheduled tests)

unwanted landing gear or landing gear doors extension/retraction

multiple tyre bursts

Navigation systems (including precision approaches system) and air data systems

total loss or multiple navigation equipment failures

total failure or multiple air data system equipment failures

significant misleading indication

significant navigation errors attributed to incorrect data or a database coding error

unexpected deviations in lateral or vertical path not caused by pilot input

problems with ground navigational facilities leading to significant navigation errors not associated with transitions from inertial navigation mode to radio mode

Oxygen

for pressurised aircraft: loss of oxygen supply in cockpit

loss of oxygen supply to a significant number of passengers, (more than 10%),including when found during maintenance or training or test purposes

 Section III - Aircraft Maintenance and RepairSection III - Aircraft Maintenance and Repair

Section III to AMC GR.40 - Aircraft Maintenance and Repair

This section is structured in such a way that the pertinent occurrences are linked with categories of activities during which they are normally observed, according to experience, in order to facilitate the reporting of those occurrences. However, this presentation must not be understood as meaning that occurrences must not be reported in case they take place outside the category of activities to which they are linked in the list.

Maintenance and Maintenance Related

Incorrect assembly of parts or components of the aircraft found during an inspection or test procedure not intended for that specific purpose.

Hot bleed air leak resulting in structural damage.

Identified burning, melting, smoke, arcing, overheating or fire occurrences.

Any defect in a critical structure or propulsion system critical part causing retirement before completion of its full life.

Any damage or deterioration, ie fractures, cracks, corrosion, delamination, disbonding, (size is by no means a reliable indication of significance) resulting from any cause (such as flutter, loss of stiffness or structural failure) to:

Critical structure (as defined by the certified type design) where such damage or deterioration exceeds allowable limits specified in the Repair Manual and requires a repair or complete or partial replacement of the structure;

secondary structure which consequently has or may have endangered the aircraft; or

the engine, propeller or rotorcraft rotor system.

Exceedance of critical structure or propulsion system critical part airworthiness limitations or maintenance requirements.

Any failure, malfunction or defect of any system or equipment, or damage or deterioration found as a result of compliance with an Airworthiness Directive or other mandatory instruction issued by a Regulatory Authority, when:

it is detected for the first time by the reporting organisation implementing compliance;

on any subsequent compliance where it exceeds the permissible limits quoted in the instruction and/or published repair/rectification procedures are not available.

Failure of any emergency system or equipment, including all exit doors and lighting, to perform satisfactorily, including when being used for maintenance or test purposes.

Non compliance or significant errors in compliance with required maintenance procedures.

Wrong assessment of a serious defect, or serious non-compliance with the Minimum Equipment List (MEL) and Technical logbook procedures.

Incorrect control or application of aircraft maintenance limitations or scheduled maintenance.

Releasing an aircraft to service from maintenance in case of any non-compliance which endangers the flight safety.

Serious damage caused to an aircraft during maintenance activities due to incorrect maintenance or use of inappropriate or unserviceable ground support equipment that requires additional maintenance actions.

Any occurrence where the human performance, including fatigue of personnel, has directly contributed to or could have contributed to an accident or a serious incident.

Products, parts, appliances and materials of unknown or suspect origin.

Misleading, incorrect or insufficient maintenance data or procedures that could lead to maintenance errors, which could endanger flight safety.

Failure, malfunction or defect of ground equipment used for test or checking of aircraft systems and equipment when the required routine inspection and test procedures did not clearly identify the problem when this results in a hazardous situation, which could endanger flight safety.

Significant malfunction, reliability issue, or recurrent recording quality issue affecting a flight recorder system (such as a flight data recorder system, a data link recording system or a cockpit voice recorder system) or lack of information needed to ensure the serviceability of a flight recorder system.

 Section IV - Air Navigation Services, Aerodromes Facilities and Ground ServicesSection IV - Air Navigation Services, Aerodromes Facilities and Ground Services

Section IV to AMC GR.40 - Air Navigation Services, Aerodrome Facilities and Ground Services

Under DASR Phase 1, reporting of Air Navigation Services (ANS), Aerodrome (ADR) and Ground based occurrences using the Hazard Reporting and Tracking framework articulated within the Defence Aviation Safety Manual, and supporting procedures meets the intent of this Section.

A listing of specific Authority reportable ANS, ADR and Ground-based occurrences will be consulted / promulgated in 2018.

Reportable occurrences are those where the safety of operation was or could have been endangered or which could have led to an unsafe condition. If in the view of the reporter an occurrence did not hazard the safety of the operation but if repeated in different but likely circumstances would create a hazard, then a report should be made.

Immediate Notification of Accidents and Serious Incidents

Accidents and Serious Incidents are serious occurrences (deaths, serious injury and serious damage to aircraft and property or had a high potential/likelihood to do so due to the lack or remaining controls) require additional and immediate notification to the aviation safety investigation Authority. This immediate reporting requirement extends to any occurrence where there is an exposure to a serious risk of death, injury or damage.

The need to report an occurrence in accordance with this AMC does not immediately constitute the need to conduct Accident or Serious Incident investigation.

List of immediately notifiable occurrences. Section V is a list of accidents and serious incidents that require immediate notification to the aviation safety investigation Authority. It is possible for occurrences listed under Reportable Occurrences above, (SECTIONs I to IV), to be further categorised as serious incidents and would therefore subject to immediate notification requirements. In these instances professional judgement is required. Section V - Immediate Notification of Accidents and Serious IncidentsSection V - Immediate Notification of Accidents and Serious Incidents

Section V to AMC GR.40 - Immediate Notification of Accidents and Serious Incidents

It is possible for occurrences not listed here to be further categorised as serious incidents and therefore subject to immediate notification requirements. In this instance professional judgement is required. Categorisation of these occurrences into accidents or serious incidents, is often circumstance dependent so it is most important to note that the categorisation of any occurrence should only be finalised after a thorough examination of all the circumstances of that occurrence.

The immediate notification of Accidents and Serious Incidents should occur as soon as is reasonably practicable.

Accident:

Death of any person

Loss of an aircraft, ie unrepairable, missing or inaccessible for recovery.

Serious Incident.

The list is not exhaustive and only serves as guidance to the definition of serious incident.

Near collisions requiring an avoidance manoeuvre to avoid a collision or an unsafe situation or when an avoidance action would have been appropriate.

Controlled flight into terrain only marginally avoided.

Aborted take-offs on a closed or engaged runway, on a taxiway1 or unassigned runway.

Take-offs from a closed or engaged runway, from a taxiway2 or unassigned runway.

Landings or attempted landings on a closed or engaged runway, on a taxiway3 or unassigned runway.

Gross failures to achieve predicted performance during take-off or initial climb.

Fires and smoke in the passenger compartment, in cargo compartments or engine fires, even though such fires were extinguished by the use of extinguishing agents.

Events requiring the emergency use of oxygen by the flight crew.

Aircraft structural failures or engine disintegrations, including uncontained turbine engine failures, not classified as an accident.

Multiple malfunctions of one or more aircraft systems seriously affecting the operation of the aircraft.

Flight crew incapacitation in flight.

Fuel quantity requiring the declaration of an emergency by the pilot.

Runway incursions.

Take-off or landing incidents. Incidents such as under-shooting, overrunning or running off the side of runways.

System failures, weather phenomena, operations outside the approved flight envelope or other occurrences which could have caused difficulties controlling the aircraft.

Reporting Time

The reporting time starts from when the occurrence took place or from the time when the reporter determined that there was, or could have been, a potentially hazardous or unsafe condition. The immediate notification of Accidents and Serious Incidents should occur as soon as reasonably practicable.

The reporting period for all other occurrences that have not required immediate notification is 72 hours. Within the overall limit of 72 hours for the submission of a report, the degree of urgency should be determined by the level of hazard judged to have resulted from the occurrence. Subsequent reporting from organisations made aware of an occurrence is to be within 72 hours of initial notification.

Content of Reports

Notwithstanding other required reporting means as promulgated by other legislation, regulation or policy, reports may be transmitted in any form considered acceptable to the Authority. The amount of information in the report should be commensurate with the severity of the occurrence. Each report should at least contain the following elements, as applicable to each organisation:

Organisation details

Information necessary to identify the affected:

aircraft and / or component affected, including software version (if applicable),

ANS system,

Aerodrome.

Date and time if relevant

Summary description of the occurrence

Any other specific/ relevant information

For any occurrence involving a system or component, which is monitored or protected by a warning and/or protection system, for example: fire detection/extinguishing or separation alert, the occurrence report should always state whether such system(s) functioned properly.

Reporting Between Organisations

Requirements exist that address the reporting of data relating to unsafe or unairworthy conditions. These reporting lines are:

Production Organisation to the organisation responsible for the design;

Maintenance organisation to the organisation responsible for the design;

Maintenance organisation to operator;

Operator to organisation responsible for the design;

Production organisation to production organisation;

Design organisation to production organisation.

The ‘Organisation responsible for the design’ is a general term, which can be any one or a combination of the following organisations:

Holder of a Military Type-certificate (MTC) of an Aircraft, Engine or Propeller.

Holder of a Military Supplemental Type-certificate (MSTC) on an Aircraft, Engine or Propeller.

Holder of an Approved Design.

NOTE: In the ADF context this usually means the Systems Program Office (SPO) with embedded Military Type-certificate holder, Total Logistics Support Contractor, or both. If it can be determined that the occurrence has an impact on or is related to other aircraft types then the holders of such approval/authorisation should be informed. Figure 1 presents a simplified scheme of reporting lines for Initial and Continuing Airworthiness organisations.

 

Figure 1 - Reporting Lines

GR.60 Oversight and enforcement

Regulated entities must cooperate with DASA with a view to assuring compliance with the DASR.

For the purposes of the implementation of paragraph (a), regulated entities must conduct investigations, including ramp inspections, and must take any measure to prevent the continuation of a non-compliance.

In order to facilitate the taking of appropriate enforcement action by competent authorities, regulated entities shall exchange information on identified infringements with DASA. 

When objective evidence is found showing non-compliance with the applicable requirements of the DASR, DASA will issue a finding which shall be classified as follows: GMGM

GM GR.60(d) – Oversight and enforcement (AUS)

An interpretation of Finding Levels in the context of DASR 147 are as follows: 

DASR 147 Level 1 Finding – A non-compliance that ‘lowers the safety standard and seriously hazards flight safety’ in a DASR 147 environment would result from a critical failure of a training product that degrades training outcomes impacting airworthiness. Examples might include a failure to follow established training procedures that have a direct impact to training outcomes, significant deviation from approved training product, significant unapproved changes to the training organisation, or awarding training outcomes that have not been fully achieved.

DASR 147 Level 2 Finding – A non-compliance that ‘lowers the safety standard and possibly hazards flight safety’ in a DASR 147 environment would result from a major failure of a training product or a major failure to comply with training governance requirements that has the possibility to degrade training outcomes impacting airworthiness. Examples might include a deviation in training processes that impacts training outcomes or a major deviation from approved training product.

DASR 147 Level 3 Finding – A non-compliance, or potential problem, that ‘could lower the safety standard and possibly hazard flight safety’ in a DASR 147 environment would result from a minor failure of a training product or minor failure to comply with training governance requirements. Examples might include minor errors in documentation or minor procedural deviations that if left untreated could manifest into a lowering of safety standards, or a minor failure to achieve training governance requirements.

DASR Level 1 finding - Any non-compliance with the DASR requirements which lowers the safety standard and seriously hazards flight safety.

DASR Level 2 finding - Any non-compliance with the DASR requirements which lowers the safety standard and possibly hazards flight safety.

DASR Level 3 finding - Any non-compliance with the DASR requirements or potential problem that could lower the safety standard and possibly hazards flight safety.

After receipt of notification for a Level 1 or Level 2 finding, the regulated entity shall, to the satisfaction of DASA and within a period agreed by DASA: GMGM

GM GR.60(e) – Oversight and enforcement

Root-cause Analysis

It is important that the analysis does not primarily focus on establishing who or what caused the non-compliance but why it was caused. Establishing the root causes of a non-compliance often requires an overarching view of the events and circumstances that led to it, to identify all possible systemic and contributing factors (regulatory, human factors, organisational, managerial, cultural, technical, etc) in addition to the direct factors. A narrow focus on single events or failures, or the use of a simple method such as fault tree, to identify the chain of events that led to the non-compliance may not properly reflect the complexity of the issue. This may then give rise to the risk that important factors that are required to be addressed in order to prevent recurrence will be ignored.

Such inappropriate or partial root-cause analysis often leads to defining ‘quick fixes’ addressing the symptoms of the non-compliance only. A peer review of the results of the root-cause analysis may increase its reliability and objectivity.

A system description of the organisation considering organisational structures, processes and their interfaces, procedures, staff, equipment, facilities and the environment in which the organisation operates will support both effective root-cause (reactive) and hazard (proactive) analysis.

Corrective Actions

Corrective action is the action to eliminate or mitigate the root causes and prevent recurrence of an existing detected non-compliance, or other undesirable condition or situation. Proper determination of the root cause is crucial for defining effective corrective actions to prevent recurrence.

Corrective Action Plan

The corrective action plan links individual root causes and corrective actions defining the strategy to prevent non-compliance recurrence. It documents the expected objective quality evidence required to validate the effectiveness of the corrective action and the timeline for implementation (inclusive of collective evidence to validate effectiveness) of each corrective action.

implement an immediate action to eliminate so far as is reasonably practicable (SFARP), or otherwise minimise SFARP, the Aviation Safety risk associated with the non-compliance; 

identify the root cause of the non-compliance; 

define a corrective action plan; and

demonstrate effective corrective action implementation.

After receipt of notification for a Level 3 finding, the regulated entity shall:

manage the finding internally through its own management system; and

implement action as necessary to address the non-compliance or potential problem.

Non-compliance by the regulated entity with the actions identified in DASR GR.60(e) will result in a full or partial suspension of the relevant DASR authorisation by DASA. 
 

GR.80 Flexibility provisions

(Reserved)

Where an equivalent level of protection to that attained by the application of the DASR can be achieved by other means, DASA may approve exception from those DASR.

DASA may allow a credible and defensible level of military aviation safety performance where an equivalent level of protection to that provided by the application of the DASR cannot be demonstrated, but can be supported by the application of sound risk management principles.GMGM

GM GR.80 (c) – Flexibility Provisions 

This regulation recognises that Defence is a military force that sometimes needs to operate at levels of risk greater than would be acceptable to national civil aviation authorities. Such increased risks may result from:

incomplete type certification activities without sufficient controls to achieve the safety requirements, due, for example, to:

production inconsistencies or flaws

incompatibilities between original civil/military type certifications and Defence’s Configuration, Role and Environment (CRE)

uncertainty about original certification basis requirements for long-serving legacy aircraft and aerodromes; and

an inability to obtain, for acquired aircraft, adequate disclosure of the original certification basis requirements on which Defence will base its military type certification.

operational imperatives necessitating unairworthy aircraft to be operated; that is the certificate of airworthiness is invalid.

operating imperatives necessitating operations outside the scope of the MAOC (such as for specific missions and crew compositions, specific flying orders not being able to be met).

enduring operational imperatives such as an inability to achieve desired capability outcomes whilst compliant with contemporary crash protection requirements.

The flexibility provided by this regulation allows Defence, inter alia, to operate outside a type certification basis, to operate outside the scope of the MAOC, to operate with open 'design/type certification' issue papers, as well as continued operations with known unserviceabilities, unrepaired damage or deferred maintenance, eg where the certificate of airworthiness is invalid.

This flexibility provision does not exempt Defence from a duty under the Australian Work Health and Safety (WHS) Act. Consequently, where operations under the flexibility provision are contemplated, the risks to health and safety of persons must be eliminated so far as is reasonably practicable and if this is not possible then reduced so far as is reasonably practicable in the circumstance.

DASA must acknowledge that regulated organisations may deviate from the substantive requirements laid down in this Regulation in the event of compelling operational imperatives or emergencies.GMGM

GM GR.80 (d) – Flexibility Provisions 

This regulation continues the long-standing flexibility arrangement whereby operational commanders may deviate from aviation safety requirements in an emergency or compelling circumstance. Such deviations should only be made where there is insufficient time either to seek:

permit to fly as described in DASR Subpart P, or

prior Authority approval for an exception or a reduced level of protection as provided for at GR.80 (b) and GR.80 (c) respectively.

 

Annex A: DASR parts

See menu page

DASR 21 Aircraft Design, Production and Certification

DASR 66 Military Aircraft Maintenance Licencing

DASR 139 Aerodromes

DASR 145 Requirements for Maintenance Organisations

DASR 147 Aircraft Maintenance Training Organisations.

DASR ABM Air Battle Management

DASR ACD Air Cargo Delivery

DASR Aircrew

DASR ANSP Air Navigation Service Providers

DASR AO.Gen Air Operations General

DASR ARO Authority Requirements for Air Operations

DASR AVFM Aviation Fatigue Management

DASR FSTD Flight Simulation Training Devices

DASR FT Flight Tests

DASR M Continuing Airworthiness Management

DASR MED Medical

DASR NDR Non-Defence Registered aircraft

DASR NTS Non-Technical Skills

DASR ORO Organisation Requirements for Air Operations

DASR RoA Rules of the Air.

DASR SMS Aviation Safety Management Systems

DASR SPA Specific Purpose Approval

DASR SPO Special Purpose Operations

DASR UAS Uncrewed Aircraft Systems